Research on Unbalanced Vibration Suppression Method for Coupled Cantilever Dual-Rotor System

被引:5
|
作者
Lu, Jiaqiao [1 ]
Zhang, Xin [1 ,2 ]
Pan, Xin [1 ,2 ]
Zhang, Meng [1 ]
机构
[1] Beijing Univ Chem Technol, Key Lab Engine Hlth Monitoring Control & Networki, Minist Educ, Beijing 100029, Peoples R China
[2] Beijing Univ Chem Technol, Beijing Key Lab High End Mech Equipment Hlth Moni, Beijing 100029, Peoples R China
基金
中国国家自然科学基金; 北京市自然科学基金;
关键词
dual-rotor system; unbalance; coupling vibration; self-sensitivity coefficient; automatic balance; actuator; vibration suppression; RESPONSE CHARACTERISTICS; COMPENSATION; IMBALANCE;
D O I
10.3390/machines10090758
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The cantilever dual-rotor system is a typical structure of the blade output end of the open rotor engine and the coaxial output turboshaft engine. The excessive unbalanced vibration of a coupled cantilever dual-rotor system is one of the main factors limiting the application of the above engine type. In order to accurately describe the vibration coupling effect between the dual-rotor-intermediate bearings, the unbalanced response of the cantilever dual-rotor system is analyzed, and the self-sensitivity coefficient is proposed to guide the selection of measuring points and vibration suppression experiments for the dual-rotor system. On this basis, a new online automatic balance actuator applicable to this dual-rotor system is designed, and a feasibility experiment is carried out. The experimental results indicate that: (1) The self-sensitivity coefficient can be used as the basis for the actual vibration measuring point arrangement and unbalanced vibration suppression strategy of the dual-rotor system, and the proposed step-by-step vibration suppression strategy can reduce the vibration of the dual-rotor system by more than 80%. (2) The designed online automatic balance actuator can reduce the unbalanced vibration by 53% in 3.52 s. The proposed method in this study can provide guidance for the vibration suppression of the dual-rotor system.
引用
收藏
页数:19
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